A03 No requirement for North American manufacturers
A04 Included in the Qualified Products List of the applicable Military Specification
A05 All requirements of qualification section
A07 Mechanical tensile properties
A08 Tensile properties in H1000 condition
A11 Free or controlled cold bend
A22 Embrittlement or internal residual stresses - mercurous nitrate
A23 Embrittlement or internal residual stresses - acid copper sulfate
A38 Susceptibility to intergranular attack
A40 Fluorescent penetrant inspection
A41 Magnetic particle inspection
A42 Response to heat treatment
A46 Internal quality or defects or soundness by ultrasonic evaluation
A47 Internal quality or internal cleanliness by magnetic particle inspection
A49 Bursting strength or internal hydrostatic pressure
A50 Non destructive evaluation acceptance criteria on a part by part basis to the requirements of the applicable engineering drawing
A51 Approval is dependant on first article inspection on a part by part basis. There shall be evidence of satisfactory chemical composition, mechanical properties, metallographic appearance, grain size, grain flow, ultrasonic quality, surface contamination and penetrant inspection quality in conformance with the applicable forging specification and engineering drawing requirements.
A52 Approval is dependant on first article inspection on a part by part basis. There shall be evidence of satisfactory chemical composition, mechanical properties, metallographic appearance, grain flow, grain size, ultrasonic quality, surface contamination, decarburization conditions and magnetic particle inspection quality in conformance with the applicable forging specification and engineering drawing requirements.
A53 Chemical composition and mechanical tensile properties.
A54 Stress corrosion and electrical conductivity
A56 Sensitivity and contamination
A57 Thickness and covering area
A58 Flattenability or bend and leak by pressure or eddy current
A59 Flattenability, flexibility and leakage
A60 Chemical composition, wire size and mesh size
A61 Stretch limits and permanent set, and sheave requirements for endurance testing
A62 Stress corrosion, exfoliation corrosion and electrical conductivity
A63 Bendability, flarability, leakage and corrosion resistance
A64 Flattenability, flarability, leakage and pressure
A65 Flarability, bendability and grain size
A66 Flattenability or bend and flarability
A67 Microstructure, macrostructure and grain size
A68 Chemical composition, hardenability, grain size and decarburization
A69 Bendability, flarability, leakage, corrosion resistance and grain size
A70 Flattenability, flarability, bendability and grain size
A71 Bendability, grain size and decarburization
A72 A sample of the product under review supplied to BAMPE for evaluation
A73 No new manufacturer is required
A77 Products must be listed in the "Commercial Engine, Standard Practices Manual" for G.E. Aircraft Engines.
A77 Products must be listed in the "Commercial Engine, Standard Practices Manual" for GE Aircraft Engines
A78 Acceleration 55AB008 shall be used only with Tristar's 620 series of topcoats (CMS 565-02 Gr A).
A78 Accelerator 55AB008 shall be used only with Tristar's 620 series of topcoats (BAMS 565-002 Gr. A)
A79 Acceleration IM-108 shall be used only with Crown Metro's 24F2 - series of topcoats (BAMS 565-009 TY I, Cl A, Gr A).
A79 Accelerator IM-108 shall be used only with Crown `Metro's 24F2-series of topcoats (BAMS 565-009, TY I,CL A, GR A)
A80 Approval for each P/N will be in accordance with BAERD GEN-009 for castings, BAERD GEN-008 for forgings, BAPS 188-004 for Ti-6A1-4V superplastic formed parts and BAPS 188-006 for Aluminum superplastic formed parts. BAMPE approval of a test report in compliance with an approved Bombardier Aerospace Engineering Test Plan is required. Approval of forgings applies to forgings (die, contour, hand, billet) which have individual part numbers. Hand forged billets/blocks without part numbers do not require approval on a part-by-part basis.
A81 Inspection materials shall be from the same family group. Use of penetrant, remover and developer from different manufacturers is not permitted. (For information only Ref. BAPS 176-002).
A82 Consistency grade viscosity, dropping point penetration
A83 Requirements of FDA 21 CFR 178.3570 and NSF standard 61. Bleed, evaporation, dielectric strength
A84 Viscosity and static shear strength after room temperature curing
A85 Supplier qualification requirements as per the material specification.
A86 Qualification of suppliers shall be based upon evaluation of chemical composition, radiographic inspection and mechanical properties (including fracture toughness) taken from castings from a minimum of 10 melts. A minimum of 100 tensile data points from designated areas of the castings is required.
A87 Included in the Qualified Products List of the applicable AMS
A89 Recrystallized Layer Thickness
A91 Only approved for use at Bombardier Aerospace sites.
A92 BAMPE recommends that this product is used only on business aircraft when required by the customer.
A94 Internal residual stresses/ammonia vapor
A95 Phenolic based prepregs should be excluded from primary structures and used solely where low flammability, smoke and toxicity requirements are dominant, and any design should make accommodation for the material's high variability.
A96 All requirements per specification
A97 All tests showing compliance with the requirements of the AMS-PRF-46194 specification. Table II "cleaning compound" not required.